Learjet 35 - Page 39

Leerjet 35/36 Developed for Training Purposes 2B-15
February 2007
Expanded Normal Procedures
No Smoking/Seat Belt Sign. . . . . . . . . . . . . . . . . . . . . . . . ON
Cabin Air . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
Pressurization . . . . . . . . . . . . . AUTO/ALTITUDE/RATE SET
AUTO-MAN Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO
The switch is normally in AUTO unless a malfunction hasoc-
curred.
Cabin Altitude Controller. . . . . . . . . . . . . . . . . . . . . . . . . SET
Set controller to the cruise flight level. If on a short leg, set
cabin altitude to landing field elevation.
Cabin Rate-of-Climb . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET
The 9 o’clock position provides approximately a 500 FPM
cabin altitude cabin rate.
Temp Controls . . . . . . . . . . . . . . . . . . . . . . . . . . AS DESIRED
Bleed Air Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
Emer Pressurization Switches
(if installed) . . . . . . . . . . . . . . . . . . . . . . . . . . GUARD DOWN
TOLD Data/Bugs . . . . . . . . . . . . . . . . . . . . .COMPUTED/SET
Ice Detect Lights . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKED
Emergency Gyro . . . . . . . . . . . . . . . . . . . . . . . . . . UNCAGED
CVR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TEST
Drag Chute Handle (if installed) . . . . . . . . . . . . . . . STOWED
Trim/Pitch, Roll, Yaw/Switches . . . . . . . . . . .CHECKED/SET/
.............................................................................. PRIMARY
NOTE: Check illuminated by placing an object between the
lights and windshield. Use care to prevent scratching wind-
shield when checking ice detect lights.
NOTE: Refer to AFM for minimum trim systems preflight
check.